EP0894715A3 - Engine nacelle outer cowl panel with integral track fairings and method for making same - Google Patents
Engine nacelle outer cowl panel with integral track fairings and method for making same Download PDFInfo
- Publication number
- EP0894715A3 EP0894715A3 EP98202571A EP98202571A EP0894715A3 EP 0894715 A3 EP0894715 A3 EP 0894715A3 EP 98202571 A EP98202571 A EP 98202571A EP 98202571 A EP98202571 A EP 98202571A EP 0894715 A3 EP0894715 A3 EP 0894715A3
- Authority
- EP
- European Patent Office
- Prior art keywords
- cowl panel
- outer cowl
- engine nacelle
- making same
- integral track
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
- B29C70/86—Incorporated in coherent impregnated reinforcing layers, e.g. by winding
- B29C70/865—Incorporated in coherent impregnated reinforcing layers, e.g. by winding completely encapsulated
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/34—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
- B29C70/342—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation using isostatic pressure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
- B29D24/00—Producing articles with hollow walls
- B29D24/002—Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled
- B29D24/005—Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled the structure having joined ribs, e.g. honeycomb
- B29D24/007—Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled the structure having joined ribs, e.g. honeycomb and a chamfered edge
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
- B29D99/00—Subject matter not provided for in other groups of this subclass
- B29D99/0089—Producing honeycomb structures
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D29/00—Power-plant nacelles, fairings, or cowlings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D29/00—Power-plant nacelles, fairings, or cowlings
- B64D29/02—Power-plant nacelles, fairings, or cowlings associated with wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2995/00—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
- B29K2995/0037—Other properties
- B29K2995/0087—Wear resistance
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
- B29L2031/3076—Aircrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0206—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising noise reduction means, e.g. acoustic liners
Abstract
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP07001301A EP1770011B1 (en) | 1997-07-30 | 1998-07-30 | Engine nacelle outer cowl panel |
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US5428497P | 1997-07-30 | 1997-07-30 | |
US54284P | 1997-07-30 | ||
US09/013,993 US6129311A (en) | 1997-07-30 | 1998-01-27 | Engine nacelle outer cowl panel with integral track fairings |
US13993 | 1998-01-27 |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP07001301A Division EP1770011B1 (en) | 1997-07-30 | 1998-07-30 | Engine nacelle outer cowl panel |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0894715A2 EP0894715A2 (en) | 1999-02-03 |
EP0894715A3 true EP0894715A3 (en) | 2000-04-19 |
EP0894715B1 EP0894715B1 (en) | 2007-04-25 |
Family
ID=26685519
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP98202571A Expired - Lifetime EP0894715B1 (en) | 1997-07-30 | 1998-07-30 | Engine nacelle outer cowl panel with integral track fairings and method for making same |
EP07001301A Expired - Lifetime EP1770011B1 (en) | 1997-07-30 | 1998-07-30 | Engine nacelle outer cowl panel |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP07001301A Expired - Lifetime EP1770011B1 (en) | 1997-07-30 | 1998-07-30 | Engine nacelle outer cowl panel |
Country Status (3)
Country | Link |
---|---|
US (1) | US6129311A (en) |
EP (2) | EP0894715B1 (en) |
DE (1) | DE69837640T2 (en) |
Families Citing this family (40)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9586699B1 (en) | 1999-08-16 | 2017-03-07 | Smart Drilling And Completion, Inc. | Methods and apparatus for monitoring and fixing holes in composite aircraft |
US9625361B1 (en) | 2001-08-19 | 2017-04-18 | Smart Drilling And Completion, Inc. | Methods and apparatus to prevent failures of fiber-reinforced composite materials under compressive stresses caused by fluids and gases invading microfractures in the materials |
FR2862607B1 (en) * | 2003-11-24 | 2007-03-23 | Airbus France | AIRCRAFT PARTITION FOR SEPARATING A CARGO PORTION FROM A COCKPIT OR A PASSENGER COMPARTMENT |
DE102006044093B4 (en) * | 2006-09-20 | 2009-01-22 | Airbus Deutschland Gmbh | Disk replacement to fill a window frame |
US7797944B2 (en) * | 2006-10-20 | 2010-09-21 | United Technologies Corporation | Gas turbine engine having slim-line nacelle |
US7870721B2 (en) * | 2006-11-10 | 2011-01-18 | United Technologies Corporation | Gas turbine engine providing simulated boundary layer thickness increase |
DE112007001683T5 (en) * | 2007-01-17 | 2010-01-07 | United Technologies Corporation, Hartford | Nuclear reflex nozzle for a turbofan engine |
US8408491B2 (en) | 2007-04-24 | 2013-04-02 | United Technologies Corporation | Nacelle assembly having inlet airfoil for a gas turbine engine |
US8205430B2 (en) * | 2007-05-16 | 2012-06-26 | United Technologies Corporation | Variable geometry nacelle assembly for a gas turbine engine |
US8727267B2 (en) * | 2007-05-18 | 2014-05-20 | United Technologies Corporation | Variable contraction ratio nacelle assembly for a gas turbine engine |
US8402739B2 (en) * | 2007-06-28 | 2013-03-26 | United Technologies Corporation | Variable shape inlet section for a nacelle assembly of a gas turbine engine |
US9228534B2 (en) * | 2007-07-02 | 2016-01-05 | United Technologies Corporation | Variable contour nacelle assembly for a gas turbine engine |
FR2921342B1 (en) * | 2007-09-20 | 2010-03-12 | Airbus France | LOWER REAR AERODYNAMIC FAIRING FOR AN AIRCRAFT ENGINE CLAMPING DEVICE |
US9004399B2 (en) | 2007-11-13 | 2015-04-14 | United Technologies Corporation | Nacelle flow assembly |
US8192147B2 (en) * | 2007-12-14 | 2012-06-05 | United Technologies Corporation | Nacelle assembly having inlet bleed |
US8186942B2 (en) * | 2007-12-14 | 2012-05-29 | United Technologies Corporation | Nacelle assembly with turbulators |
US8529188B2 (en) * | 2007-12-17 | 2013-09-10 | United Technologies Corporation | Fan nacelle flow control |
DE102008044759B4 (en) | 2008-08-28 | 2013-09-19 | Airbus Operations Gmbh | Support for an aircraft structural component which can be produced using the selective laser melting method |
US9188026B2 (en) * | 2008-11-26 | 2015-11-17 | Mra Systems, Inc. | Apparatus for facilitating access to a nacelle interior and method of assembling the same |
US9188025B2 (en) * | 2008-11-26 | 2015-11-17 | Mra Systems, Inc. | Apparatus for facilitating access to a nacelle interior |
US8220738B2 (en) * | 2008-11-26 | 2012-07-17 | Mra Systems, Inc. | Nacelle and method of assembling the same |
US8172176B2 (en) * | 2009-02-04 | 2012-05-08 | Spirit Aerosystems, Inc. | Integral composite slider for aircrafts |
DE102009058359A1 (en) * | 2009-12-15 | 2011-06-16 | Airbus Operations Gmbh | Force introduction fitting for lightweight components |
FR2954278B1 (en) * | 2009-12-18 | 2012-01-20 | Aircelle 7303 | SUPPORT STRUCTURE FOR THRUST INVERTER, IN PARTICULAR WITH GRIDS |
US9057286B2 (en) | 2010-03-30 | 2015-06-16 | United Technologies Corporation | Non-circular aft nacelle cowling geometry |
US8578609B2 (en) * | 2010-10-27 | 2013-11-12 | Airbus Operations S.L. | Manufacturing procedure of a part made out of a composite material introducing a geometric change in one of its faces |
GB2485183A (en) * | 2010-11-04 | 2012-05-09 | Rolls Royce Plc | Generating residual stress in hollow body during cure to deflect composite body on relaxation |
FR2970670A1 (en) * | 2011-01-26 | 2012-07-27 | Aircelle Sa | Composite part for use in nacelle of engine of aircraft, has core comprising body provided with face that comprises corners having respective round vertices, where body of core includes beveled edge inclined at angle of specific degree |
DE102011018526A1 (en) * | 2011-04-26 | 2012-10-31 | Airbus Operations Gmbh | Force introduction fitting for lightweight components |
FR2982588B1 (en) * | 2011-11-10 | 2013-11-22 | Aircelle Sa | COMPOSITE PANEL WITH INTEGRATED SAMPLING ECOPE |
US9168716B2 (en) * | 2012-09-14 | 2015-10-27 | The Boeing Company | Metallic sandwich structure having small bend radius |
US20150330254A1 (en) | 2014-05-15 | 2015-11-19 | United Technologies Corporation | Compact Nacelle With Contoured Fan Nozzle |
US10196937B2 (en) * | 2015-12-30 | 2019-02-05 | General Electric Company | Method and system for improving structural characteristics of composite component corners |
US10197007B2 (en) | 2016-01-14 | 2019-02-05 | General Electric Company | Method and system for controlling core cowl vent area |
GB2570104B (en) * | 2017-12-18 | 2021-12-29 | Composite Integration Ltd | Improved system and method for resin transfer moulding |
US10384723B2 (en) | 2017-12-19 | 2019-08-20 | Ford Global Technologies, Llc | Vehicle cross-car beam |
US11047308B2 (en) | 2018-06-29 | 2021-06-29 | The Boeing Company | Acoustic panel for thrust reversers |
CN109849370B (en) * | 2019-03-20 | 2021-12-28 | 成都联科航空技术有限公司 | Processing method of rocket/missile engine interstage connection structure |
FR3095158B1 (en) * | 2019-04-17 | 2021-04-30 | Hutchinson | Method of manufacturing a grid for a thrust reverser |
US11702982B2 (en) * | 2019-10-24 | 2023-07-18 | The Boeing Company | Blade fragment barrier for aircraft engine inlet cowl |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4533098A (en) * | 1983-06-20 | 1985-08-06 | General Electric Company | Thrust reverser attachment |
US4826106A (en) * | 1987-02-18 | 1989-05-02 | Grumman Aerospace Corporation | Advanced composite aircraft cowl |
US5239822A (en) * | 1992-01-14 | 1993-08-31 | The Boeing Company | Composite structure for thrust reverser torque box |
Family Cites Families (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2654686A (en) * | 1950-05-11 | 1953-10-06 | Northrop Aircraft Inc | Stiffened honeycomb core |
US3616112A (en) * | 1969-08-29 | 1971-10-26 | Balsa Dev Corp | Balsa wood core in a laminated structural sandwich |
US3658974A (en) * | 1970-05-28 | 1972-04-25 | Nasa | Method of forming shapes from planar sheets of thermosetting materials |
US4030290A (en) * | 1974-11-06 | 1977-06-21 | The Boeing Company | Jet engine thrust reverser |
US4026105A (en) * | 1975-03-25 | 1977-05-31 | The Boeing Company | Jet engine thrust reverser |
US4043522A (en) * | 1975-12-22 | 1977-08-23 | The Boeing Company | Common pod for housing a plurality of different turbofan jet propulsion engines |
US4232513A (en) * | 1977-10-19 | 1980-11-11 | Rolls-Royce Limited | Pressure relief panel for aircraft powerplant |
US4235303A (en) * | 1978-11-20 | 1980-11-25 | The Boeing Company | Combination bulk absorber-honeycomb acoustic panels |
US4539244A (en) * | 1979-08-06 | 1985-09-03 | Rohr Industries, Inc. | Honeycomb noise attenuation structure |
US4421201A (en) * | 1981-09-29 | 1983-12-20 | The Boeing Company | High efficiency broadband acoustic resonator and absorption panel |
US4463552A (en) * | 1981-12-14 | 1984-08-07 | United Technologies Corporation | Combined surge bleed and dust removal system for a fan-jet engine |
DE3280226D1 (en) * | 1982-09-29 | 1990-09-13 | Boeing Co | DOOR DEVICE FOR REVERSE BLOCKING. |
US4495764A (en) * | 1983-05-26 | 1985-01-29 | The United States Of America As Represented By The Secretary Of The Air Force | Integrated insulation wall assembly |
AT384189B (en) * | 1983-10-10 | 1987-10-12 | Fischer Gmbh | BUILDING PLATE |
US4852805A (en) * | 1983-12-30 | 1989-08-01 | The Boeing Company | Hybrid thrust reverser cascade basket and method |
US4680216A (en) * | 1984-09-04 | 1987-07-14 | United Technologies Corporation | Method for stabilizing thick honeycomb core composite articles |
US4600619A (en) * | 1984-12-31 | 1986-07-15 | The Boeing Company | Continuously wound filament structure for use in noise attenuation element |
US4779240A (en) * | 1985-04-29 | 1988-10-18 | Xecutek Corporation | Ultrasonic sensor system |
US4759513A (en) * | 1986-09-26 | 1988-07-26 | Quiet Nacelle Corporation | Noise reduction nacelle |
US4825644A (en) * | 1987-11-12 | 1989-05-02 | United Technologies Corporation | Ventilation system for a nacelle |
US5054281A (en) * | 1989-09-25 | 1991-10-08 | Rohr Industries, Inc. | Gas turbine engine compartment vent system |
DE4130620C2 (en) * | 1991-09-14 | 1994-10-06 | Eurocopter Deutschland | Process for bending a flat object with a honeycomb structure |
US5428498A (en) | 1992-09-28 | 1995-06-27 | Xerox Corporation | Office environment level electrostatic discharge protection |
DE4343904C3 (en) * | 1993-12-22 | 1999-11-04 | Mtu Muenchen Gmbh | Component made of fiber-reinforced composite material with a protective layer against erosion |
US5498462A (en) * | 1994-04-01 | 1996-03-12 | Hexcel Corporation | High thermal conductivity non-metallic honeycomb |
GB9424495D0 (en) * | 1994-12-05 | 1995-01-25 | Short Brothers Plc | Aerodynamic low drag structure |
-
1998
- 1998-01-27 US US09/013,993 patent/US6129311A/en not_active Expired - Lifetime
- 1998-07-30 EP EP98202571A patent/EP0894715B1/en not_active Expired - Lifetime
- 1998-07-30 EP EP07001301A patent/EP1770011B1/en not_active Expired - Lifetime
- 1998-07-30 DE DE69837640T patent/DE69837640T2/en not_active Expired - Lifetime
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4533098A (en) * | 1983-06-20 | 1985-08-06 | General Electric Company | Thrust reverser attachment |
US4826106A (en) * | 1987-02-18 | 1989-05-02 | Grumman Aerospace Corporation | Advanced composite aircraft cowl |
US5239822A (en) * | 1992-01-14 | 1993-08-31 | The Boeing Company | Composite structure for thrust reverser torque box |
Also Published As
Publication number | Publication date |
---|---|
EP0894715A2 (en) | 1999-02-03 |
DE69837640D1 (en) | 2007-06-06 |
EP1770011A3 (en) | 2007-06-27 |
EP1770011A2 (en) | 2007-04-04 |
EP0894715B1 (en) | 2007-04-25 |
US6129311A (en) | 2000-10-10 |
DE69837640T2 (en) | 2008-01-03 |
EP1770011B1 (en) | 2011-05-25 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP0894715A3 (en) | Engine nacelle outer cowl panel with integral track fairings and method for making same | |
EP0986041A3 (en) | Selective release label sheet | |
EP0833060A3 (en) | Blade for axial fluid machine | |
EP1520698A3 (en) | Method of controlling printing on both surfaces of a sheet of print media | |
EP1067210A3 (en) | Method for providing a hard carbon film on a substrate and electric shaver blade | |
EP0728589A3 (en) | Recording apparatus | |
EP1006600A3 (en) | Separator structure for a fuel cell and method for making same | |
EP0828036A3 (en) | Horizontal-roofing roof and mounting method thereof | |
EP0869259A3 (en) | Method for repairing a turbine vane damaged tip | |
EP0805108A3 (en) | Aircraft engine thrust mount | |
EP0867364A3 (en) | Compensation apparatus for main rotor torque | |
EP0962406A3 (en) | Apparatus for adjusting the relative position of side-walls for guiding containers, in machines for forming arrays of said containers | |
EP0381339A3 (en) | Constructional panels | |
EP2275617A3 (en) | Locking system for floorboards | |
EP1010570A3 (en) | Vehicle control system | |
EP1298286A3 (en) | Guide vane assembly | |
EP1366912A3 (en) | Load and feed apparatus for solid ink | |
WO2000003079A3 (en) | Method for printing fibrous textile materials according to the ink jet printing technique | |
CA2269811A1 (en) | Printer or copier with two printing units and method for the operation of such an apparatus | |
EP1004230A3 (en) | Control of an agricultural vehicle | |
EP0962409A3 (en) | Modular air jet array for feeding flat sheets | |
EP0730966A3 (en) | Ink container and manufacturing method therefor | |
EP0900614A3 (en) | Method and apparatus for forming the edge of an airfoil | |
EP0950530A3 (en) | Recording apparatus | |
EP0853059A3 (en) | Device for selectively feeding sheets from two trays in an office machine |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
AK | Designated contracting states |
Kind code of ref document: A2 Designated state(s): DE FR GB |
|
AX | Request for extension of the european patent |
Free format text: AL;LT;LV;MK;RO;SI |
|
PUAL | Search report despatched |
Free format text: ORIGINAL CODE: 0009013 |
|
PUAF | Information related to the publication of a search report (a3 document) modified or deleted |
Free format text: ORIGINAL CODE: 0009199SEPU |
|
PUAL | Search report despatched |
Free format text: ORIGINAL CODE: 0009013 |
|
RTI1 | Title (correction) |
Free format text: ENGINE NACELLE OUTER COWL PANEL WITH INTEGRAL TRACK FAIRINGS AND METHOD FOR MAKING SAME |
|
AK | Designated contracting states |
Kind code of ref document: A3 Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE |
|
AX | Request for extension of the european patent |
Free format text: AL;LT;LV;MK;RO;SI |
|
AX | Request for extension of the european patent |
Free format text: AL;LT;LV;MK;RO;SI |
|
R17D | Deferred search report published (corrected) |
Effective date: 20000419 |
|
RTI1 | Title (correction) |
Free format text: ENGINE NACELLE OUTER COWL PANEL WITH INTEGRAL TRACK FAIRINGS AND METHOD FOR MAKING SAME |
|
17P | Request for examination filed |
Effective date: 20001006 |
|
AKX | Designation fees paid |
Free format text: DE FR GB |
|
17Q | First examination report despatched |
Effective date: 20021115 |
|
RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: SPIRIT AEROSYSTEMS, INC. |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): DE FR GB |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D |
|
REF | Corresponds to: |
Ref document number: 69837640 Country of ref document: DE Date of ref document: 20070606 Kind code of ref document: P |
|
ET | Fr: translation filed | ||
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
26N | No opposition filed |
Effective date: 20080128 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20110727 Year of fee payment: 14 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20110727 Year of fee payment: 14 Ref country code: DE Payment date: 20110727 Year of fee payment: 14 |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20120730 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: ST Effective date: 20130329 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20120731 Ref country code: DE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20130201 Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20120730 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R119 Ref document number: 69837640 Country of ref document: DE Effective date: 20130201 |